GB2165374B - Gas turbine engine control - Google Patents

Gas turbine engine control

Info

Publication number
GB2165374B
GB2165374B GB08515972A GB8515972A GB2165374B GB 2165374 B GB2165374 B GB 2165374B GB 08515972 A GB08515972 A GB 08515972A GB 8515972 A GB8515972 A GB 8515972A GB 2165374 B GB2165374 B GB 2165374B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
engine control
thrust
engine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB08515972A
Other versions
GB8515972D0 (en
GB2165374A (en
Inventor
Ronald Sheldon Carpenter
Frederick John Pineo
William Lawrence Gazzola
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of GB8515972D0 publication Critical patent/GB8515972D0/en
Publication of GB2165374A publication Critical patent/GB2165374A/en
Application granted granted Critical
Publication of GB2165374B publication Critical patent/GB2165374B/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

In one form of the present invention, the thrust of a gas turbine engine is inferred. If a droop in thrust is predicted, components of the engine are modulated in response to restore thrust.
GB08515972A 1984-10-01 1985-06-24 Gas turbine engine control Expired GB2165374B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/656,567 US4581889A (en) 1984-10-01 1984-10-01 Gas turbine engine control

Publications (3)

Publication Number Publication Date
GB8515972D0 GB8515972D0 (en) 1985-07-24
GB2165374A GB2165374A (en) 1986-04-09
GB2165374B true GB2165374B (en) 1988-09-01

Family

ID=24633600

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08515972A Expired GB2165374B (en) 1984-10-01 1985-06-24 Gas turbine engine control

Country Status (7)

Country Link
US (1) US4581889A (en)
JP (1) JPS6185560A (en)
DE (1) DE3523144A1 (en)
FR (1) FR2571098B1 (en)
GB (1) GB2165374B (en)
IT (1) IT1200656B (en)
SE (1) SE458548B (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5072580A (en) * 1989-02-27 1991-12-17 United Technologies Corporation System for operating gas turbine jet engine with fan damage
US4959955A (en) * 1989-02-27 1990-10-02 United Technologies Corporation Method of operating gas turbine engine with fan damage
DE8902635U1 (en) * 1989-03-04 1989-04-13 Filztuchverwaltungs GmbH, 6082 Mörfelden-Walldorf Device for inserting cored wires into a wire link belt
JPH02267328A (en) * 1989-03-20 1990-11-01 General Electric Co <Ge> Controller of gas turbine engine and controlling method
US5197280A (en) * 1989-03-20 1993-03-30 General Electric Company Control system and method for controlling a gas turbine engine
US5267435A (en) * 1992-08-18 1993-12-07 General Electric Company Thrust droop compensation method and system
US5694760A (en) * 1996-07-19 1997-12-09 General Electric Company Cumbustor lean flameout control
US5732546A (en) * 1996-07-19 1998-03-31 General Electric Company Transient turbine overtemperature control
US6250877B1 (en) 2000-07-19 2001-06-26 General Electric Co. Steam turbine controller having method and apparatus for providing variable frequency regulation
JP2002274783A (en) * 2001-03-19 2002-09-25 Furukawa Co Ltd Outrigger device for on-vehicle crane
WO2008063152A2 (en) * 2006-10-12 2008-05-29 United Technologies Corporation Turbofan engine
US8490404B1 (en) * 2012-02-28 2013-07-23 General Electric Company Sensor-based performance-seeking gas turbine engine control
WO2016189712A1 (en) 2015-05-27 2016-12-01 株式会社Ihi Jet engine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB812557A (en) * 1955-10-10 1959-04-29 Westinghouse Electric Int Co Improvements in or relating to gas turbine power plants
GB789999A (en) * 1955-05-25 1958-01-29 Gen Electric Improvements in and relating to engine acceleration control systems
US2971326A (en) * 1956-01-23 1961-02-14 Bendix Corp Temperature limiting system for gas turbine exhaust area control
US2979889A (en) * 1956-09-18 1961-04-18 Bendix Corp Temperature-modified exhaust nozzle scheduling controller for a gas turbine engine
US2955412A (en) * 1957-01-17 1960-10-11 Gen Motors Corp Gas turbine nozzle control
US3019604A (en) * 1959-01-19 1962-02-06 Gen Motors Corp Turbojet thrust computer
US3747344A (en) * 1970-07-20 1973-07-24 Gen Electric Variable nozzle area control system
US4139887A (en) * 1977-04-28 1979-02-13 United Technologies Corporation Dynamic compensation for multi-loop controls
US4258545A (en) * 1978-06-15 1981-03-31 General Electric Company Optimal control for a gas turbine engine
DE2930956C2 (en) * 1979-07-31 1985-07-18 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Control method for a surface-adjustable thrust nozzle of a bypass gas turbine jet engine with afterburner

Also Published As

Publication number Publication date
SE458548B (en) 1989-04-10
JPH0532578B2 (en) 1993-05-17
FR2571098B1 (en) 1993-05-07
US4581889A (en) 1986-04-15
FR2571098A1 (en) 1986-04-04
DE3523144A1 (en) 1986-04-10
SE8503172D0 (en) 1985-06-26
GB8515972D0 (en) 1985-07-24
IT1200656B (en) 1989-01-27
IT8521319A0 (en) 1985-06-27
JPS6185560A (en) 1986-05-01
GB2165374A (en) 1986-04-09
SE8503172L (en) 1986-04-02

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19940624